DE3431583C2 - - Google Patents
Info
- Publication number
- DE3431583C2 DE3431583C2 DE3431583A DE3431583A DE3431583C2 DE 3431583 C2 DE3431583 C2 DE 3431583C2 DE 3431583 A DE3431583 A DE 3431583A DE 3431583 A DE3431583 A DE 3431583A DE 3431583 C2 DE3431583 C2 DE 3431583C2
- Authority
- DE
- Germany
- Prior art keywords
- control
- force
- output signal
- summation element
- rod
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 238000006073 displacement reaction Methods 0.000 claims description 23
- 238000009966 trimming Methods 0.000 claims description 10
- 230000003321 amplification Effects 0.000 claims description 5
- 238000003199 nucleic acid amplification method Methods 0.000 claims description 5
- 230000008030 elimination Effects 0.000 claims description 2
- 238000003379 elimination reaction Methods 0.000 claims description 2
- 238000010586 diagram Methods 0.000 description 5
- 230000001133 acceleration Effects 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 238000012937 correction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005672 electromagnetic field Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 230000036316 preload Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 238000012549 training Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
- G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
- B64C27/58—Transmitting means, e.g. interrelated with initiating means or means acting on blades
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
- G05D1/0061—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Mechanical Engineering (AREA)
- Mechanical Control Devices (AREA)
- Toys (AREA)
- Position Input By Displaying (AREA)
- Force Measurement Appropriate To Specific Purposes (AREA)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19843431583 DE3431583A1 (de) | 1984-08-28 | 1984-08-28 | Vorrichtung zur automatischen beseitigung von steuerkraftfehlern bei luftfahrzeugen, insbesondere hubschraubern |
DE8585109650T DE3585770D1 (de) | 1984-08-28 | 1985-07-31 | Steuer-vorrichtung fuer luftfahrzeugen, insbesonder hubschraubern. |
EP85109650A EP0179209B1 (de) | 1984-08-28 | 1985-07-31 | Steuer-Vorrichtung für Luftfahrzeugen, insbesonder Hubschraubern |
US06/769,874 US4607202A (en) | 1984-08-28 | 1985-08-27 | Apparatus for automatically eliminating control force errors in aircraft, especially helicopters |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19843431583 DE3431583A1 (de) | 1984-08-28 | 1984-08-28 | Vorrichtung zur automatischen beseitigung von steuerkraftfehlern bei luftfahrzeugen, insbesondere hubschraubern |
Publications (2)
Publication Number | Publication Date |
---|---|
DE3431583A1 DE3431583A1 (de) | 1986-03-13 |
DE3431583C2 true DE3431583C2 (xx) | 1989-12-21 |
Family
ID=6244080
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19843431583 Granted DE3431583A1 (de) | 1984-08-28 | 1984-08-28 | Vorrichtung zur automatischen beseitigung von steuerkraftfehlern bei luftfahrzeugen, insbesondere hubschraubern |
DE8585109650T Expired - Fee Related DE3585770D1 (de) | 1984-08-28 | 1985-07-31 | Steuer-vorrichtung fuer luftfahrzeugen, insbesonder hubschraubern. |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8585109650T Expired - Fee Related DE3585770D1 (de) | 1984-08-28 | 1985-07-31 | Steuer-vorrichtung fuer luftfahrzeugen, insbesonder hubschraubern. |
Country Status (3)
Country | Link |
---|---|
US (1) | US4607202A (xx) |
EP (1) | EP0179209B1 (xx) |
DE (2) | DE3431583A1 (xx) |
Families Citing this family (32)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2565882B2 (fr) * | 1984-06-13 | 1987-09-18 | Centre Nat Rech Scient | Dispositif de liaison a plusieurs degres de liberte |
FR2590044B1 (fr) * | 1985-09-27 | 1988-01-29 | Applic Mach Motrices | Dispositif de commande electrique motorise |
FR2591189B1 (fr) * | 1985-12-05 | 1988-05-27 | Rabouyt Denis | Dispositif d'assistance au pilotage d'aeronefs a voilure tournante. |
US4696445A (en) * | 1986-09-18 | 1987-09-29 | United Technologies Corporation | Collective control system for a helicopter |
JPH0226301A (ja) * | 1988-07-12 | 1990-01-29 | Teijin Seiki Co Ltd | サーボ制御装置 |
US5058825A (en) * | 1989-02-09 | 1991-10-22 | Denis Rabouyt | Steering aid for rotor aircraft |
FR2647922B1 (fr) * | 1989-05-31 | 1993-12-31 | Sextant Avionique | Dispositif de commande electromecanique utilisable pour le pilotage d'un vehicule |
WO1995012153A1 (en) * | 1992-10-06 | 1995-05-04 | Honeywell Inc. | Position dependent rate dampening in an active hand controller |
FR2708112B1 (fr) * | 1993-07-22 | 1995-09-01 | Ratier Figeac Soc | Dispositif de commande à manche de pilotage, notamment mini-manche asservi pour aéronef. |
US5522568A (en) * | 1993-11-09 | 1996-06-04 | Deka Products Limited Partnership | Position stick with automatic trim control |
US5489830A (en) * | 1994-09-09 | 1996-02-06 | Mcdonnell Douglas Corporation | Control system with loadfeel and backdrive |
FR2728537A1 (fr) * | 1994-12-21 | 1996-06-28 | Eurocopter France | Dispositif pour l'actionnement d'un organe commande pour un aeronef, tel que notamment un helicoptere, a commandes de vol electriques |
FR2728536A1 (fr) * | 1994-12-22 | 1996-06-28 | Eurocopter France | Systeme de palonnier a gradient d'effort pour helicoptere |
FR2728541A1 (fr) * | 1994-12-22 | 1996-06-28 | Eurocopter France | Systeme de manche cyclique a gradient d'effort pour helicoptere |
JPH0924898A (ja) * | 1995-07-12 | 1997-01-28 | Teijin Seiki Co Ltd | 小型航空機の操縦装置 |
JP3091743B1 (ja) | 1999-03-30 | 2000-09-25 | 株式会社コミュータヘリコプタ先進技術研究所 | 操縦装置 |
US6519929B2 (en) | 2001-04-30 | 2003-02-18 | Honeywell International, Inc. | System and method for controlling the deployment of jet engine thrust reversers |
US6526744B2 (en) | 2001-04-30 | 2003-03-04 | Honeywell International Inc. | System and method for controlling the stowage of jet engine thrust reversers |
US6439504B1 (en) | 2001-06-15 | 2002-08-27 | Honeywell International, Inc. | System and method for sustaining electric power during a momentary power interruption in an electric thrust reverser actuation system |
US6681559B2 (en) | 2001-07-24 | 2004-01-27 | Honeywell International, Inc. | Thrust reverser position determination system and method |
US6684623B2 (en) | 2002-02-27 | 2004-02-03 | Honeywell International, Inc. | Gearless electric thrust reverser actuators and actuation system incorporating same |
US6622963B1 (en) | 2002-04-16 | 2003-09-23 | Honeywell International Inc. | System and method for controlling the movement of an aircraft engine cowl door |
US6679458B2 (en) * | 2002-06-10 | 2004-01-20 | The Boeing Company | Split detent tactile cueing vehicle control system |
FR2847352B1 (fr) * | 2002-11-18 | 2005-01-28 | Airbus France | Systeme de commandes de vol electriques pour aeronef comportant une detection de couplages oscillatoires de pilotage et organe de pilotage pour un tel systeme |
US7463956B2 (en) | 2003-07-03 | 2008-12-09 | The Boeing Company | Constant vertical state maintaining cueing system |
CN102001443B (zh) * | 2007-08-08 | 2013-05-29 | 莫戈公司 | 一种复合弹簧 |
US8074940B2 (en) * | 2007-08-08 | 2011-12-13 | Moog Inc. | Control stick adapted for use in a fly-by-wire flight control system, and linkage for use therein |
FR2920744B1 (fr) * | 2007-09-07 | 2010-04-09 | Eurocopter France | Verin de compensation pour commande de vol de giravion |
FR2943619B1 (fr) * | 2009-03-30 | 2012-08-10 | Sagem Defense Securite | Systeme de commande de vol pour aeronef, comportant une biellette pourvue de capteur |
FR3034750B1 (fr) * | 2015-04-13 | 2017-12-08 | Airbus Helicopters | Systeme de commande d'un rotor de giravion, giravion equipe d'un tel systeme et methode de commande associee |
DE102018104192A1 (de) | 2018-02-23 | 2019-08-29 | Autogyro Ag | Tragschrauber |
EP4393814A1 (en) * | 2022-12-29 | 2024-07-03 | Airbus Defence and Space, S.A.U. | Active trim system of a flight control system of an aircraft |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3476335A (en) * | 1967-05-19 | 1969-11-04 | Sperry Rand Corp | Pseudo control stick steering system for aircraft having a damper system |
US3478990A (en) * | 1967-10-31 | 1969-11-18 | Us Navy | Apparatus for resisting control stick deflection |
US3463423A (en) * | 1968-02-16 | 1969-08-26 | Martin Marietta Corp | Electromechanical force feel system for aircraft control stick |
US3700995A (en) * | 1971-05-20 | 1972-10-24 | United Aircraft Corp | Trim reference for helicopter feel augmentation system |
US4106728A (en) * | 1977-01-17 | 1978-08-15 | Sperry Rand Corporation | Fail safe force feel system |
US4228386A (en) * | 1978-06-02 | 1980-10-14 | Sperry Corporation | Aircraft servoactuator apparatus |
US4345195A (en) * | 1979-12-13 | 1982-08-17 | Sperry Corporation | Strapdown multifunction servoactuator apparatus for aircraft |
GB2135796B (en) * | 1983-02-28 | 1986-07-09 | United Technologies Corp | Variable trim-engagement system |
-
1984
- 1984-08-28 DE DE19843431583 patent/DE3431583A1/de active Granted
-
1985
- 1985-07-31 EP EP85109650A patent/EP0179209B1/de not_active Expired - Lifetime
- 1985-07-31 DE DE8585109650T patent/DE3585770D1/de not_active Expired - Fee Related
- 1985-08-27 US US06/769,874 patent/US4607202A/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
DE3585770D1 (de) | 1992-05-07 |
DE3431583A1 (de) | 1986-03-13 |
EP0179209B1 (de) | 1992-04-01 |
EP0179209A3 (en) | 1987-07-22 |
US4607202A (en) | 1986-08-19 |
EP0179209A2 (de) | 1986-04-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8110 | Request for examination paragraph 44 | ||
D2 | Grant after examination | ||
8364 | No opposition during term of opposition | ||
8327 | Change in the person/name/address of the patent owner |
Owner name: EUROCOPTER DEUTSCHLAND GMBH, 8012 OTTOBRUNN, DE |
|
8339 | Ceased/non-payment of the annual fee |